小型固定翼无人机Aerosonde建模与控制仿真
本实验以小型固定翼无人机 Aerosonde 为对象，通过动力学分析，建立了固定翼飞机非线性动力学模型，并利用 matlab/simulink 对所建模型进行了仿真。本实验选择的控制方法为 PID 控制，其物理意义明确，适用范围广。利用matlab/simulink 对设计的飞行控制系统进行仿真，可以看出，在 PID 控制下，飞机能有较好的飞行效果。
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